[0001] This invention relates to a composite material having corrosion resistance at high
temperatures and a method for its manufacture and, more particularly, to the material
and method for producing a metal foil material for use in catalytic converters.
[0002] As well known, exhaust gases discharged from motor vehicles may contain halogen gases,
halogen compounds and lead compounds, for example, Cl
2, Br
2, PbCl
2, C
2H
2Cl
2, and C
2H
2Br
2, besides unburnt noxious gases including carbon monoxide, hydrocarbons and the like,
and components or parts made of ferrous base alloy material for exhaust system of
the motor vehicles or the like, for example, heat exchangers, air ducts, or containers,
tend to be subjected to corrosion by the noxious compounds as described above. Moreover,
halogen compounds (e.g. salt) employed for preventing freezing during cold seasons
are liable to enter these components of ferrous base alloy material, which are then
corroded by the atmosphere containing halogen gas produced when the halogen compounds
are decomposed at high temperatures.
[0003] It has been known to use metal foil materials as substrates with an appropriate catalyst
coating in place of ceramic material substrates. Such metal foil material has been
made from steel sheets containing aluminum and also chromium in order to have the
desired corrosion resistance at high temperature. These FeCrAl alloys, however, are
difficult to produce by conventional rolling and annealing processes. To overcome
the processing difficulties, it has been suggested, as in EP-A-475 420, to produce
the foil by a rapid solidification processing method; but such processing is expensive
and requires very precise controls. It has also been suggested to dip the stainless
steel in a molten bath of aluminum or aluminum alloy to apply melt-plating on the
surface of the stainless steel (U.S. Patents No. 3,907,611, 3,394,659 and 4,079,157).
This stainless steel with the aluminum is then subjected to a heat treatment to form
an alloy layer having Fe and Al as the main components. Still further, surface layers
of aluminum in binder materials, as described in U.S. Patent No. 4,228,203, have also
been suggested. However, in all of these applications the control of the processing
parameters is complex and expensive; and the resulting foil has not proven, in many
cases, to have the desired corrosion/oxidation resistance at elevated temperatures.
[0004] Accordingly, the present invention provides for a composite metal foil material and
method of manufacture typically for catalytic converters having corrosion resistance
at high temperatures and resistance against oxidation in an exhaust gas atmosphere.
Further, the composite material is easily and economically manufactured for high volume
applications.
[0005] Briefly described, in accordance with the invention, a metal foil material is made
by producing a three layer material with the two outside layers being essentially
identical and chosen from the group consisting of stainless steel materials and aluminum
materials; and the central layer being made from the material not chosen for the outside
layers, as for example, a central layer of stainless steel sandwiched between two
thinner outer layers of aluminum or aluminum alloys. The three-layer materials, having
a relatively thin starting thickness, are pressure rolled together to further reduce
the thickness of the layer materials, to metallurgically bond the layer materials
to each other to form a composite multilayer metal material having a thickness such
that the composite material can be pressure rolled to the desired foil thickness without
the necessity of any heat treatment operations. Such composite is pressure rolled
to this desired foil thickness, and then is diffusion heat treated at a temperature
between 900°C and 1200°C for a period of time to cause diffusion of the various constituents
in the layers of the composite material throughout the foil. The composite forms a
material, with the complete presence of the constituents of the aluminum layer and
the stainless steel layers dispersed throughout the total foil material thereby providing
for the superior corrosion/oxidation resistance at high temperatures. The chosen composition
and thickness of these starting materials will provide for a foil material with a
known finished composition. The fact that no heating of the composite material is
needed prior to reaching the desired foil thickness greatly increases the ability
to manufacture the material with acceptable material yields In long continuous lengths.
[0006] Other objects, advantages and details of the novel material and method of manufacture
of this invention appear in the detailed description of the preferred embodiments
of the invention, the detailed description referring to the drawings in which:
Figure 1 shows a side elevation view diagrammatically illustrating the bonding method
of this invention;
Figure 2 shows the composite material of this invention after bonding;
Figure 3 diagrammatically shows the material of this invention after diffusion heat
treatment;
Figure 4 shows the material used in a catalytic converter; and
Figure 5 shows a photomicrograph of the material of Figure 3.
[0007] In accordance with the novel and improved method and material of this invention,
a central layer 10 of ferrous material is sandwiched between two outer layers 12 and
14 of aluminum or aluminum alloy material. The three layers are passed between a pair
of pressure rolls 16 in a conventional rolling mill 18. The layers are squeezed together
with sufficient force to be reduced in thickness, and metallurgically bonded together
along interfaces 20 and 22 between the metal layers to form a composite multilayer
metal material 24 as shown in Figure 2. The material is then continuously rolled to
the desired foil thickness and thermally reacted into a foil sheet 50 as will be explained
in detail below.
[0008] Typically, the central layer 10 comprises a ferritic stainless steel with 16 to 24
wt. percent Cr, and the balance Fe with the S content less than 0.003 wt. percent.
Examples of such ferritic stainless steels are 430, 434 and 446 stainless steels with
controlled sulfur content. Preferably, top and bottom layers 12 and 14 are of the
same thickness and material, and are composed of essentially pure aluminum although
aluminum alloys could also be used.
[0009] It is to be understood that the invention could equally well be practised with a
central relatively thin layer of aluminum or aluminum alloys, and top and bottom layers
of the ferritic stainless steel material.
[0010] In a preferred embodiment having excellent high temperature oxygen corrosion resistance,
it has been found desirable to have a final chemistry in the final material 50 after
thermal reaction (to be explained in detail below) of between 18 to 20 wt. percent
Cr, at least 5 wt. percent Al and the balance Fe. Additionally, small amounts of rare
earth metals, for example, Ce, Y, and Er, may be added to either of the metals forming
the composite to further increase high temperature corrosion resistance. An example
of such an embodiment is where a layer of 434 stainless steel, having a thickness
typically of between 0.045 and 0.070 inch (1.1 to 1.8 mm), is bonded to essentially
pure aluminum top and bottom layers having a thickness typically of between 0.004
and 0.007 inch (0.1 to 0.18 mm) thereby yielding a bonded composite of approximately
0.015 to 0.025 inch (0.38 to 0.6 mm)as shown in Figure 3. One typical example results
in a composite of about 84 percent stainless steel and a top and bottom layer of aluminum
of about 8 percent each. The initial starting thicknesses of the layers have been
chosen to determine two important material characteristics of the final composite.
The first is to determine the ultimate chemistry of the final composite after thermal
reaction, and the second is to provide a bonded composite which is capable of being
reasonably continuously rolled to a desired gauge after bonding without the need of
any thermal treatment which could cause the formation of intermetallics of the metal
constituents. This second item is particularly important in being able to produce
the material economically in large production quantities.
[0011] Accordingly, the composite 24 is cold rolled by conventional means from the bonding
gauge to a foil thickness typically of about 0.002 inch (about 0.05 mm). This finish
rolled foil is then thermally reacted or heat treated at a temperature between 900°C
and 1200°C, and preferably about or above 1100°C, for between 1 minute and 60 minutes
or longer to provide for diffusion of the various constituents in the composite throughout
the foil material. That is, after this heating operation, the microstructure of the
foil will not be a three layer structure but instead a uniform solid solution alloy.
The heating can be done in a vacuum, reducing atmosphere or air. The desirability
of heating above 1100°C is the fact that such heating eliminates the formation of
undesirable Kirkendall voids, and ensures that all iron aluminide intermetallics are
dissolved. The occurrence of Kirkendall voids is also minimized by keeping the sulfur
content of the composite, and specifically the stainless steel component, to extremely
low levels (preferably less than 0.003 wt. percent). These Kirkendall voids can cause
premature failure of the foil in fatigue loading which easily can result when such
foil is used as a catalytic converter substrate.
[0012] The oxidation resistance of the foil material of the present invention is further
enhanced by the formation of a thin layer of an aluminum oxide whisker network on
the metal surface typically done in an additional heating operation at a temperature
between 900°C and 1100°C in air although it may be done as part of the diffusion heating
step. The oxide layer prevents the metal from further oxidation. During thermal cycling
when used as a catalytic converter substrate foil material, the oxide layer tends
to crack and separate from the base material directly below the surface which results
in this material further oxidizing. To reduce the separation of the surface oxide
layer from the base material below and to increase adhesion, a small amount of rare
earth elements (between 0.01 and 0.10 wt. percent) is preferably added to the foil
material. In the present invention, this rare earth metal addition may be made by
the addition of such metal(s) in either the starting aluminum or ferrous materials.
These rare earth metal element additions, combined with extremely low sulfur content,
further minimize any Kirkendall voids.
[0013] In order to give greater appreciation of the advantages of the invention, the following
examples are given:
Example I
[0014] A continuous strip of completely annealed 434 stainless steel having a thickness
of 0.060 inch (1.5 mm) was cleaned and brushed. This strip was sandwiched between
two continuous strips of cleaned aluminum foil of 0.006 inch (0.15 mm) each and roll
bonded in a single operation to yield a solid state metallurgically bonded three layer
composite of 0.020 inch (0.05 mm) as described in U.S. Patent No. 2,753,623 to which
the reader is referred for more detailed information. This composite material continuous
strip was cold rolled on a conventional rolling mill in multiple passes until the
desired gauge of 0.002 inch (0.05 mm) was achieved. This foil material was then heated
to 1100° C in vacuum for 60 minutes to diffuse all the aluminum into the stainless
steel base, thereby forming a complete uniform solid solution foil material. This
foil material showed approximate chemical composition of 75 wt. percent Fe, 20 wt.
percent Cr, and 5 wt. percent Al. The metal materials were of uniform concentration
throughout the foil.
Example II
[0015] This example was carried out identically to Example I above except the starting center
strip used was pure aluminum having a thickness of 0.012 inch (0.3 mm) and the top
and bottom strip layers were of 434 stainless steel each having a thickness of 0.030
inch (0.76 mm). The finished foil material after heat treatment had the same uniform
solid solution chemical composition as set forth in Example I above.
Example III
[0016] This example was carried out identically to Example I above except the 434 stainless
steel was replaced by a stainless steel of the following composition: 20 wt. percent
Cr, 0.015 wt. percent Ce, 0.004 wt. percent La, 0.009 wt. percent Ni, 0.002 wt. percent
S and the balance Fe with the unavoidable impurities of Mn and Si. This foil material
after heat treatment had a uniform solid solution chemical composition approximately
of 73.3 wt. percent Fe, 18.2 wt. percent Cr and 6.7 wt. percent Al for the major constituents
with S and rare earth metals in the desired range.
Example IV
[0017] This example was carried out identically to Example III above except the furnished
foil material was further heat treated in air at 960°C for 20 hours to produce the
alumina whisker network. Such alumina whisker network is desirable for applying ceramic
wash coat on the foil substrate as commonly practiced for catalytic converter manufacture.
[0018] Accordingly, the foil for use as a substrate in catalytic converters provided by
the process of this invention is typically provided with a alumina whisker network
on the surface of the foil. This alumina whisker network (not shown) has a ceramic
wash coat, as is known in the art, applied on the foil substrate (not shown), and
such catalyst sheet 51 (with whisker network and wash coat) is positioned on a frame
52 to form a catalytic converter unit 54 as shown in Figure 4.
[0019] The novel process and article produced by method of the present invention provides
for a foil material for use in catalytic converters with good corrosion resistance
at elevated temperatures. The material is easily and economically manufactured having
a selectively predetermined desired chemical composition. The chemical composition
is uniform throughout the foil sheet.
1. A method for making a foil substrate material for catalytic converters comprising
the steps of:
providing a layer of a first material chosen from the group consisting of chromium
containing ferrous metals and aluminum and aluminum alloys, sandwiching said layer
of first material between first and second layers of a second material chosen from
the group consisting of chromium containing ferrous metals and aluminum and aluminum
alloys not chosen for the first material, metallurgically bonding said layers together
by reducing the thickness of said layers thereby forming a multilayer composite material
of said first and second materials, reducing the thickness of the composite material
to a desired thickness and heating said composite material at a temperature between
900°C and 1200°C for a sufficient period of time to cause diffusion of metal constituents
of said layers throughout the composite thereby providing a uniform solid solution
material for the foil substrate.
2. A method as claimed in claim 1, wherein metallurgical bonding by reducing thickness
is effected by pressure rolling, and reducing thickness to the desired thickness is
carried out by further pressure rolling without thermal treatment that would cause
formation of intermetallic constituents of the first and second materials.
3. The method according to claim 2, wherein the thicknesses of the layers of said first
and second materials are chosen so that the composite formed from them can be easily
pressure rolled to the desired thickness for the foil substrate without a thermal
treatment.
4. The method according to claim 2, wherein said first material is a ferritic stainless
steel sheet having an initial thickness of between 0.045 and 0.070 of an inch (about
1.1 to 1.8 mm) and said second material is essentially pure Al with each layer having
an initial thickness of between 0.004 and 0.007 of an inch (about 0.1 to 0.18 mm).
5. A method according to claim 1 or claim 2, wherein said first material is a ferritic
stainless steel and said second material is aluminum.
6. The method according to any one of claims 1 to 5, wherein said heating of said composite
is carried out at about or above 1100°C.
7. The method according to any one of claims 1 to 6, wherein said time for heating said
composite is between 1 and 60 minutes.
8. The method according to any one of claims 1 to 7, wherein the chemical composition
of the uniform solid solution material is between 18 and 20 wt. percent Cr, at least
5 wt. percent Al and the balance Fe.
9. The method according to claim 8, wherein the chemical composition further includes
a small amount of rare earth metals.
10. The method according to claim 9, wherein said small amount of rare earth metals is
between 0.01 and 0.10 wt. percent.
11. The method according to any one of claims 8 to 10, wherein the chemical composition
has a content of S of less than 0.003 wt. percent.
12. A method according to any one of claims 1 to 11, wherein said material is further
heat treated in air at a temperature between 900°C and 1100°C for sufficient time
to form a thin surface layer of an aluminum oxide whisker network.
13. A foil substrate material made according to the method of any one of claims 1 to 12.
14. The use, in the manufacture of a foil substrate material composed of a uniform solid
solution, of the steps of:
providing a layer of a first material chosen from the group consisting of chromium
containing ferrous metals and aluminum and aluminum alloys, sandwiching said layer
of first material between first and second layers of a second material chosen from
the group consisting of chromium containing ferrous metals and aluminum and aluminum
alloys not chosen for the first material, metallurgically bonding said layers together
by reducing the thickness of said layers thereby forming a multilayer composite material
of said first and second materials, reducing the thickness of the composite material
to a desired thickness and heating said composite material at a temperature between
900°C and 1200°C for a sufficient period of time to cause diffusion of the metal constituents
of said layers throughout the composite to form the uniform solid solution.